McDonnell-Douglas MD-11 vs. Lockheed Martin F-35 Lightning II

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McDonnell-Douglas MD-11 versus Lockheed Martin F-35 Lightning II
61.20 m 200 ft 10 in length 15.67 m 51 ft 4 in
17.6 m 57 ft 9 in height 4.33 m 14 ft 2 in
51.6 m 169 ft 4 in wingspan 10.7 m 35 ft 1 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 40,000 lb
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 40,000 lb
285,990 kg 630,400 lb MTOW 31,800 kg 70,000 lb
13,231 km 7,147 nm range 1,380 mi 1,200 nm
961 km/h 597 mph cruise speed 520 kt 302 mph
Max 410 passengers capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.